SAW Modulators and Light Steering Methods

ABSTRACT

An electro-holographic light field generator device is disclosed. The light field generator device has an optical substrate with a waveguide face and an exit face. One or more surface acoustic wave (SAW) optical modulator devices are included within each light field generator device. The SAW devices each include a light input, a waveguide, and a SAW transducer, all configured for guided mode confinement of input light within the waveguide. A leaky mode deflection of a portion of the waveguided light, or diffractive light, impinges upon the exit face. Multiple output optics at the exit face are configured for developing from each of the output optics a radiated exit light from the diffracted light for at least one of the waveguides. An RF controller is configured to control the SAW devices to develop the radiated exit light as a three-dimensional output light field with horizontal parallax and compatible with observer vertical motion.

RELATED APPLICATIONS

This application is a Divisional of U.S. patent application Ser. No.15/883,802, filed on Jan. 30, 2018, which claims the benefit under 35USC 119(e) of U.S. Provisional Application 62/452,281, filed Jan. 30,2017, U.S. Provisional Application 62/453,041, filed Feb. 1, 2017, andU.S. Provisional Application No. 62/468,455, filed on Mar. 8, 2017,which are incorporated herein by this reference in their entirety.

This application is related to:

U.S. application Ser. No. 15/883,811 filed on Jan. 30, 2018, entitled“Electro-Holographic Light Field Generators and Displays,” now U.S.Patent Publication No.: 2018-0217414 A1; and International Applicationnumber PCT/US2018/015930 filed on Jan. 30, 2018, entitled,“ELECTRO-HOLOGRAPHIC LIGHT FIELD GENERATORS AND DISPLAYS,” nowInternational Application Publication No.: WO 2018/140939.

All of the afore-mentioned applications are incorporated herein by thisreference in their entirety.

BACKGROUND OF THE INVENTION

Existing three dimensional (3D) display architectures utilize a varietyof techniques including scanning, space-multiplexing, and steeredillumination, among others. One architecture, electro-holographicdisplays, relies principally on diffractive phenomena, but it has notyet delivered on the promise of high image quality and compactness.Examples of electro-holographic displays are described in: Jason Geng,Three-dimensional display technologies, Advances in Optics andPhotonics, 5, 456-535 (2013). (see pp. 508-516) and Yijie Pan et al., AReview of Dynamic Holographic Three-Dimensional Display: Algorithms,Devices, and Systems, IEEE Transactions on Industrial Informatics,12(4), 1599-1610 (August 2016).

A primary disadvantage of existing electro-holographic displays, andtheir constituent modulators, is their low product of display size andspatial frequency; this product is sometimes called the space-bandwidthproduct. A large modulator, or a modulator capable of being tiled into alarge direct-view display, is desirable because it obviates the need forintermediate scanners or large output lenses. A high spatial fringefrequency is desirable because it increases the field of view of thedisplay: diffraction angle increases with line pairs/mm. Pixel-basedspatial light modulators (SLMs) suffer from low space-bandwidth productbecause they are typically impractically small (with areas on the orderof 1 cm²), and have pixels typically much larger than the wavelength oflight. Similarly, existing acousto-optical modulators (AOMs) have smalldeflection angles and small active areas. For example, the MIT SpatialImaging Group Mark II holographic video display employed 18mirror-scanned TeO₂ AOMs to provide a 30° view angle, an image volume of150 millimeters (mm)×75 mm×150 mm, and 144 vertical scan lines, asdescribed in St.-Hilaire et al., Advances in holographic video, Proc.SPIE 1914, Practical Holography VII: Imaging and Materials, vol. 188,pp. 188-96, (1993).

An alternative to the forgoing optical modulation modalities is asurface acoustic wave (SAW) optical modulator, a device category thatprovides controllable sub-holograms from which a light field can beconstructed. Briefly, in a SAW optical modulator, a waveguide, patternedon an optical substrate, carries a time-varying diffracting region thatis formed by index changes due to the substrate's piezoelectric effectunder radio frequency (RF) excitation (e.g., at 300 MHz), as described,for example, in Onural et al., “New high-resolution display device forholographic three-dimensional video: principles and simulations,”Optical Engineering, vol. 33(3), pp. 835-44 (1994); Matteo et al.,Collinear Guided Wave to Leaky Wave Acoustooptic Interactions inProton-Exchanged LiNbO3 Waveguides, IEEE Trans. on Ultrasonics,Ferroelectrics, and Frequency Control, 47(1), 16-28 (January 2000);Smalley et al., Anisotropic leaky-mode modulator for holographic videodisplays, Nature, 498, 313-317 (20 Jun. 2013); U.S. Pat. App. Publ. US2014/0300695, FULL-PARALLAX ACOUSTO-OPTIC/ELECTRO-OPTIC HOLOGRAPHICVIDEO DISPLAY.

One type of SAW modulator is the guided-to-leaky-mode device fabricatedusing lithium niobate as described, for example, in Hinkov et al.,Collinear Acoustooptical TM-TE Mode Conversion in Proton ExchangedTi:LiNbO3 Waveguide Structures, J. Lightwave Tech., vol. 6(6), pp.900-08 (1988); Smalley et al., Anisotropic leaky-mode modulator forholographic video displays, Nature, vol. 498, pp. 313-317 (2013), hereinafter “Smalley”; McLaughlin et al., Optimized guided-to-leaky-modedevice for graphics processing unit controlled frequency division ofcolor, Appl. Opt., vol. 54(12), pp. 3732-36 (2015); Qaderi et al.,Leaky-mode waveguide modulators with high deflection angle for use inholographic video displays, Opt. Expr., vol. 24(18), pp. 20831-41(2016), hereinafter “Qaderi”; and Savidis et al., Progress infabrication of waveguide spatial light modulators via femtosecond lasermicromachining, Proc. of SPIE Vol. 10115, 2017. The surface acousticwave interacts with input light and thereby causes at least some of thelight to change from a guided mode within the waveguide to a leaky modethat exits the waveguide.

A feature of SAW modulators is their inherently diffractive, rather thanpixelated, nature, and their potential for high frequency bandwidth,which provides the benefit of higher space-bandwidth product (and, thus,practical combinations of diffractive fan angle and modulator area).

SUMMARY OF THE INVENTION

Existing electro-holographic 3D displays that use SAW modulators havelimitations. The exit angle of the fan of light for SAW modulators istypically less than 20 degrees. Thus, embodiments of the presentinvention augment SAW modulators with optical enhancements that increasethe exit angle of the fan of exit light emitted from the SAW modulators.

Additionally, embodiments are also disclosed that include optics forconditioning the light exiting from the modulators. Various optics andlocations for the optics are disclosed.

In general, according to one aspect, the invention features a surfaceacoustic wave optical modulator. The modulator comprises a substrate, atransducer for generating a surface acoustic wave in the substrate, awaveguide in the substrate for guiding radiation through the substrateuntil the radiation is diffracted from the waveguide by the surfaceacoustic wave, the radiation exiting the substrate at an exit face.Finally, an optic is provided on this exit face.

In embodiments, the optic is transmissive. It might be a diffractiveoptic or grating. Another option is a refractive optic, such as aconcave lens or convex lens.

In one set of embodiments, the optic is formed on an end face of thesubstrate. In other cases, the optic is formed on a distal face of thesubstrate.

In still other cases, an array of the optics is provided.

In many of these cases, the optic is used to increase an exit angle fanof the light from the substrate. Nevertheless, it is helpful togenerally condition the exiting light such as to form a beam, focus thelight and/or create diverging light.

In general, according to another aspect, the invention features a methodfor steering light. The method comprises coupling light into a waveguidein a substrate, generating a surface acoustic wave in the substrate thatdiffracts light from the waveguide, conditioning a light exiting fromthe substrate with an optic on an exit face of the substrate.

In general, according to another aspect, the invention features asurface acoustic wave modulator. It comprises a substrate, a transducerfor generating a surface acoustic wave in the substrate, a waveguide inthe substrate for guiding radiation through the substrate until theradiation is diffracted from the waveguide by the surface acoustic wave.The radiation then exits the substrate at an exit face after beingreflected by another face of the substrate.

In one example, an edge cut angle of an end face relative to a proximalface of the substrate is obtuse. In this case, the light might exitthrough a distal face.

In another example, an edge cut angle of an end face relative to aproximal face of the substrate is acute. In this case, the light mightexit through the proximal face.

In one embodiment, the light is reflected by an end face is coated to bereflective.

In general, according to another aspect, the invention features a methodfor steering light. The method comprises coupling light into a waveguidein a substrate, generating a surface acoustic wave in the substrate thatdiffracts light from the waveguide, and reflecting the light at a faceof the substrate to exit at another face of the substrate.

In general, according to another aspect, the invention features asurface acoustic wave modulator. The modulator comprises a substratehaving at least two adjacent non-orthogonal faces, a waveguide fortransmitting light, and a transducer for generating a surface acousticwave to diffract light from the waveguide toward one of the faces.

In embodiments, an edge cut angle of an end face relative to a proximalface of the substrate is obtuse or acute. An optic could also beprovided on one of the faces.

In general, according to another aspect, the invention features a methodfor forming a surface acoustic wave modulator. The method comprisesforming a substrate and a waveguide in the substrate for transmittinglight, providing a transducer for generating a surface acoustic wave todiffract light from the waveguide, and forming the substrate with atleast two adjacent non-orthogonal faces.

The above and other features of the invention including various noveldetails of construction and combinations of parts, and other advantages,will now be more particularly described with reference to theaccompanying drawings and pointed out in the claims. It will beunderstood that the particular method and device embodying the inventionare shown by way of illustration and not as a limitation of theinvention. The principles and features of this invention may be employedin various and numerous embodiments without departing from the scope ofthe invention.

BRIEF DESCRIPTION OF THE DRAWINGS

In the accompanying drawings, reference characters refer to the sameparts throughout the different views. The drawings are not necessarilyto scale; emphasis has instead been placed upon illustrating theprinciples of the invention. Of the drawings:

FIG. 1A is a schematic side view of a prior art SAW optical modulator(“SAW device”);

FIG. 1B is a schematic partial side view of a SAW device as in FIG. 1A,illustrating dimensional and angular relationships between beamstraversing a substrate of the SAW device;

FIG. 1C is a schematic side view of a SAW device as in FIG. 1A,depicting the effects of Fresnel reflections at interfaces of the SAWdevice;

FIG. 2A is a schematic side view of a proposed SAW device having anangled end face as an exit face;

FIG. 2B is a schematic side view of a portion of a proposed SAW deviceshowing extremal deflection angles of diffracted light within the SAWdevices and corresponding extremal rays of exit light for the extremaldeflection angles, where the extremal rays of exit light in FIG. 2B areemitted at a distal face of the SAW device;

FIG. 2C is a schematic side view of a portion of a proposed SAW deviceas in FIG. 2B, with the addition of a transmissive optic such as agrating placed at the distal face;

FIG. 3 is a schematic side view of a portion of another proposed SAWdevice, showing rays of diffracted light transmitting through thesubstrate of the SAW device and towards a diffraction grating as thetransmissive optic, attached to a distal face of the substrate;

FIG. 4 is a schematic plot of the decreasing spatialfrequency/decreasing deflection of the grating as a function ofposition;

FIGS. 5A and 5B show schematic side views of a portion of other proposedSAW devices that include powered refractive elements, such as a concaveoptic, to increase the deflection angle, and convex optics;

FIG. 6 is a ray trace that shows the rays of radiation of diffractedlight and exit light for the SAW device of FIG. 5, and shows how thedeflection angle is increased with the use of the grating or therefractive optic;

FIG. 7A shows a ray trace of a beam of diffracted light traversing aprior art SAW modulator device;

FIGS. 7B-7N show ray traces of beams of diffracted light traversing SAWmodulators with different end face geometries according to the presentinvention;

FIG. 8A shows a proximal face of a proposed light field generatordevice, where a partial array of SAW modulators within the light fieldgenerator device is also shown;

FIG. 8B shows a distal face of the light field generator device in FIG.8A, which shows detail for a two dimensional array of output optics ofthe SAW modulators within the light field generator device;

FIG. 8C is a schematic cross-section of a light field generator deviceas in FIGS. 8A and 8B, showing a SAW modulator constructed withdiverging diffractive lens output optics;

FIG. 9 is a schematic cross-section of a light field generator device asin FIGS. 8A and 8B, showing a SAW modulator constructed with convergingdiffractive lens output optics;

FIG. 10 is a schematic cross-section of a light field generator deviceas in FIGS. 8A and 8B, showing a SAW modulator constructed withdiffractive lens output optics;

FIG. 11A is a schematic cross-section of a light field generator deviceas in FIGS. 8A and 8B, where a SAW modulator having a single outputoptic at an end face of the SAW modulator functions as an exit face ofthe light field generator device;

FIG. 11B is a schematic cross-section of a light field generator withtwo output optics at the end face;

FIG. 12 illustrates a process for creating a SAW device that minimizesseparation between waveguide and the distal/exit face;

FIGS. 13A and 13B are diagrams that illustrate time multiplexing oflight and/or RF signal inputs to a light field generator deviceincluding one or more SAW devices and optical splitter of light to theSAW devices from one source;

FIG. 14 is a schematic section taken through planes of a prior artholographic display system;

FIG. 15 shows an electro-holographic 3D display formed from a stack oflight field generator devices, where the light field generator devicesinclude SAW devices having angled end faces;

FIGS. 16A and 16B show electro-holographic 3D having different stackingarrangements of light field generator devices than in FIG. 15;

FIG. 17 shows a 3D display system that includes an electro-holographic3D display and other components for powering and controlling theelectro-holographic 3D display, where the display is formed from adual-column stack of light field generator devices;

FIG. 18A is an enlarged top view of the prior art SAW device in FIG. 1A,where the enlarged top view shows a layout of transducer fingers of aninterdigital transducer (IDT) within the SAW device;

FIGS. 18B-18G are enlarged views of proposed SAW devices showingdifferent layouts of transducer fingers, where: FIGS. 18B and 18C arecross-sectional top views of a SAW device showing an optical waveguidechannel with transducers located on either side of, straddling, thewaveguide; FIG. 18D is a cross-sectional side view of the SAW devices inFIGS. 18B and 18C; FIG. 18E is a top cross-sectional view of a SAWdevice showing several multimode optical waveguide channels patternedwithin the SAW device; FIG. 18F is a cross-sectional top view ofmultiple multi-mode waveguide paths within a SAW device that are fed bya common source of illumination; and FIG. 18G is a cross-sectional sideview of SAW devices in either of the embodiments of FIGS. 18E and 18F.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The invention now will be described more fully hereinafter withreference to the accompanying drawings, in which illustrativeembodiments of the invention are shown. This invention may, however, beembodied in many different forms and should not be construed as limitedto the embodiments set forth herein; rather, these embodiments areprovided so that this disclosure will be thorough and complete, and willfully convey the scope of the invention to those skilled in the art.

As used herein, the term “and/or” includes any and all combinations ofone or more of the associated listed items. Further, the singular formsand the articles “a”, “an” and “the” are intended to include the pluralforms as well, unless expressly stated otherwise. It will be furtherunderstood that the terms: includes, comprises, including and/orcomprising, when used in this specification, specify the presence ofstated features, integers, steps, operations, elements, and/orcomponents, but do not preclude the presence or addition of one or moreother features, integers, steps, operations, elements, components,and/or groups thereof. Further, it will be understood that when anelement, including component or subsystem, is referred to and/or shownas being connected or coupled to another element, it can be directlyconnected or coupled to the other element or intervening elements may bepresent.

Unless otherwise defined, all terms (including technical and scientificterms) used herein have the same meaning as commonly understood by oneof ordinary skill in the art to which this invention belongs. It will befurther understood that terms, such as those defined in commonly useddictionaries, should be interpreted as having a meaning that isconsistent with their meaning in the context of the relevant art andwill not be interpreted in an idealized or overly formal sense unlessexpressly so defined herein.

It is to be understood that many materials and design choices areavailable to the engineer in implementing the teachings describedherein, and all of them are subsumed within the scope of the presentinvention. Thus, while lithium niobate as a substrate material isdiscussed, for heuristic convenience, as a suitable material, a personof ordinary skill in the art will appreciate that various materials areavailable to the engineer, and that lithium niobate is merely exemplary,as are various crystal orientations, such as x-cut and y-cut, andwaveguide architectures, such as planar, ridge, rib, embedded, immersed,and bulged. Methods described herein may be advantageously performedusing waveguides in y-cut, x-propagating lithium niobate, due to itshigh efficiency of electrical to mechanical transduction. Doping, suchas resulting in MgO-doped lithium niobate, may be employedadvantageously, in some cases, to reduce photorefractive damage.

SAW Optical Modulator Architecture

FIG. 1A shows an exemplary prior art SAW device or modulator 100. It canbe used to deflect light of the same or different colors/wavelengths 101a, 101 b, 101 c from a guided mode by different angles simultaneously.Due to fabrication, material, and power constraints, the angular rangeis ordinarily extremely limited, however, largely by the mode overlapbetween the guided mode and the SAW. As described herein, using eitherdiffractive or refractive optics, there are methods for increasing thisangular distribution, in ways that are essentially angle magnifiers.

The device 100 comprises a substrate 120 in which or on which anacousto-optic waveguide 102 has been formed. The input light 101 a, 101b, and 101 c at one or more wavelengths (λ₁, λ₂, λ₃) enters waveguide102. Typically, an in-coupling device 106 is provided to couple theinput light 101 carried in an optical fiber, for example, into thewaveguide 102. Examples of in-coupling devices 106 include in-couplingprisms, gratings, or simply butt-coupling techniques between the opticalfiber and the waveguide 102. The input light 101 is launched into aguided mode upon entry into the waveguide 102. Commonly, the TE(transverse electric) mode is guided.

In such a SAW device 100, the slab waveguide 102 is typically created ina lithium niobate substrate 120 by proton-exchange. Interdigitaltransducers 110 are written on an aluminum side of the substrate 120.The transducers 110 induce surface acoustic waves 140 in the substrate120 that propagate along the waveguide 102. Such transducers 110 areoften driven electrically, e.g. using a 300-500 MHz radio frequency (RF)input signal 130.

The light interacts with the surface acoustic wave 140. The result ofthis interaction between the surface acoustic wave 140 and the light inthe waveguide 102 is that a portion of the guided light ispolarization-rotated out of the guided mode and into a leaky mode havingthe transverse magnetic (TM) polarization. The light then exits thewaveguide 102 as polarized leaky-mode or diffracted light 162 and enterssubstrate 120. At some point this diffracted light 162 exits thesubstrate 120, either through the substrate's side as in FIG. 1A or itsbottom as in FIG. 1B, as exit light 150 at an exit angle fan α. Therange of possible exit angles comprises the angular extent, or exitangle fan, of the exit light 150.

Due to fabrication, material, and power constraints, the angular rangeof exit angles α is ordinarily very limited. Qaderi (2016), for example,reports that a total exit angle α of approximately 20° can be achieved,which is significantly lower than the field of view of contemporary 2-Ddisplays that approach 180°.

FIG. 1B shows the relationships between different beams of diffractedlight 162 in the SAW device 100 of FIG. 1A to illustrate its limitedangular range. Once diffracted from the waveguide 102, the diffractedlight 102 propagates through thickness h of substrate 120. Diffractedlight 162-1 propagates through the substrate 120 at deflection angle C.The deflection angle Cis measured relative to grazing, such as proximalface 160 of substrate 120. The diffracted light 162 exits distal face168 of substrate 120 at a distance h/tan φ₁ from the point 165 normal towhere the light left the waveguide 102.

Depending on the crystal phase and the values of the overlap integralfor the waveguide mode, using a higher or lower RF drive frequency ofthe RF input signals 130, a higher deflection angle φ may be achieved.This is illustrated by diffracted light 162-2, at deflection angle ϕ₂ toproximal face 160 of substrate 120. Thus, as might be expected, thefinite thickness h of substrate 120 gives rise to a spatial variation ofwhere the beams of diffracted light 162 impinge upon distal face 168 ofsubstrate 120. The distance from the point normal 165 to the point ofincidence 199 of diffracted light beam 162-1 on distal face 168 shall bereferred to herein as the “finite substrate propagation displacement”182. This range of possible diffraction angles ϕ and the correspondingexit angle α, i.e., the exit fan, of the exit light 150 is generallylimited due to fabrication, material, and power constraints.

Additionally, the high refractive index contrast between the substratematerial forming the SAW modulator and the ambient medium 105 (typicallyair) leads to significant Fresnel reflections. These Fresnel reflectionsreduce the wall plug efficiency of modulator 100, and also lead to straylight in a display in which each pixel might include a separate SAWmodulator 100, thereby reducing the visual contrast of the imagery.Additionally, there is a possibility of total internal reflection, whichprevents the modulator from working at all in certain configurations.

FIG. 1C illustrates the effect of Fresnel reflections at successiveinterfaces between substrate 120 of SAW device 100 and ambient medium105. These Fresnel reflections are indicated in FIG. 1C as Fresnelreflected components 164 and give rise to stray exit light 174 and otherproblems.

Here, radiation 101 in the form of input light is introduced atin-coupling device 106. Within waveguide 102, the input light 101 isdiffracted by the surface acoustic wave 140 as diffracted light 162. Thediffracted light 162 impinges upon distal face 168 as an exit face, atan angle θ₁. The diffracted beam 162 is transmitted through the distalface 168 as exit light 150, which exits the substrate 120 through thedistal face 168 at exit angle α. The exit light 150 is the primaryintended signal to be transmitted out the SAW device 100.

However, the index discontinuity at the distal face 168 will also createa Fresnel reflected component 164. The Fresnel reflected component 164retraverses the substrate 120, with a portion emitted as stray exitlight 174 at proximal face 160, in one example. Several successivereflections are depicted at angles θ₂ and θ₃ at proximal face 160 andend face 170, respectfully, in examples. As a result, stray exit light174 exits the substrate 120 at unwanted locations and/or output faces.

Existing electro-holographic displays using SAW devices have attemptedto increase the angular subtense/exit angle α of the exit light 150(field of view) in various ways. In examples, these ways include:experimentally optimizing various modulator parameters to increase theuseful bandwidth of the RF driver such as waveguide depth and IDT design(in published systems, the output angle is a function of IDT drivefrequency); using edge-emitting modulators having “right-angle” edges;doubling the exit angle fan via waveguides on both sides of the wafer,and/or by demagnification (i.e. using a large lens to demagnify an areaof numerous modulators to provide a smaller visible display area havinglarger field of view). But it does not appear that any of these methodsare adequate to achieve an exit angle fan such as 30° or more to as highas 90° or more in any sort of flat form-factor. Other conventionalapproaches are based on building a 3D display using a diffractive lensarray including the diffractive-patch version of integral photographysuch as in J. H. Kulick, et al., Partial pixels: a three-dimensionaldiffractive display architecture, JOSA A, 12(1), 73-83 (1995), and D.Fattal et al., A multi-directional backlight for a wide-angle,glasses-free three-dimensional display, Nature 495, p 348-351 (21 Mar.2013); both of which are incorporated herein by reference in theirentireties.

Embodiments of the present invention are disclosed herein below thatprovide improved SAW devices 200. These improved SAW devices increasethe angular extent of the exit angle α of the exit light 150 as comparedto existing SAW devices 100.

FIG. 2A shows a proposed SAW device 200 utilizing different approachesfor increasing the exit angle α of the exit light 150 as compared toprior art SAW devices 100. These approaches include providing an angledend face 170 and/or placing a transmissive optic 180 such as a gratingon an exit face of the SAW device 200 to add divergence to the exitingrays of exit light 150.

In more detail, input light 101 enters the substrate 120 via thein-coupling device 106 at the input end 340 and travels through thesubstrate 120 in the waveguide 102 as a wave of guided light 301. Whenthe surface acoustic waves 140 produced by the interdigital transducer110 interact with the guided light 301, the light 301 is diffracted andcoupled into a leaky mode, which is no longer guided by the waveguide102. The light of the leaky mode leaves the waveguide 102 and ultimatelyexits the substrate 120 as exit light 150.

The illustrated SAW device 200 shows a number of innovations that can beused separately or in conjunction with each other in order to improvethe performance of the SAW device 200 such as by increasing thedivergence of the exiting rays of exit light 150. One of thoseinnovations is a non-orthogonal end face 170. Specifically, in oneexample, an end face 170 is fabricated or machined at a non-right anglerelative to the proximal face 160 and/or the distal face 168 of thesubstrate 120. A second innovation is to include a transmissive optic180, such as a diffractive optic or grating or refractive optic, withinor upon an exit face, which is the distal face 168 in the illustrateddevice 200. The transmissive optic 180 might be patterned within/uponthe exit faces during fabrication of the SAW device 200, in one example.

In more detail, the end face 170 of the substrate 120 is planar andangled by an edge cut angle β relative to the proximal face 160. Theedge cut angle β is measured from the plane of the proximal face 160 tothe end face 170. The edge cut angle β is typically chosen such that adeflection of at least half of the available cone of the deflectionangle φ, or φ/2, is normal or near normal to the distal face 168 of thesubstrate 120 after the diffracted light 162 reflects off of the endface 170. Diffracted light 162 that reflects off of an exit face, suchas end face 170, is referred to as reflected diffracted light 162′. Thereflected diffracted light 162′ is then directed toward the transmissiveoptic 180, such as a grating. In certain embodiments of the invention, areflective substance such as a metal coating or dielectric coating maybe placed on the end face 170 to increase reflectivity and thus theintensity of the reflected diffracted light 162′ traveling toward theoptic or grating 180. As the light 162′ interacts with the grating 180,the light is dispersed, increasing the overall exit angle α of the exitlight 150.

In one embodiment, the transmissive optic 180 is a subwavelength gratingthat is deposited or patterned on or otherwise fabricated on theexit/distal face 168 of the substrate 120 of the SAW device 200. As iswell known, a diffraction grating uses perturbations of the refractiveindex of different materials or dopants, such as: etched grid lines,deposited grid lines, etched holes, deposited cylinders, or othertechniques, to alter the k-vector of the light. The standard gratingequation states that the spatial frequency of the grating will alter themomentum, such that the following relation holds:

k _(initial) −k _(final) =k _(grating)

Insofar as the foregoing standard grating equation is a vector equation,it shows that the grating interaction changes the direction of thelight.

As discussed above, there is a finite distance, referred to herein asthe finite substrate propagation displacement 182 (introduced inconnection with FIG. 1B), between where the light is deflected by thesurface acoustic wave 140 from the waveguide 102 and where it impingeson the proposed angle-enhancing grating 180. This distance 182 leads toa spatial spread in the exit angle α of the exit light 150 for differentdeflection angles φ.

In FIGS. 2B and 2C, on the other hand, when the rays traverse thegrating (or other transmissive optic 180), extremal deflection angles φ₁and φ₂ of the diffracted light 162-1 and 162-2 may be mapped to extremalemergent rays of exit light 150-1 and 150-2. In both FIGS. 2B and 2C, φ₁and φ₂ denote the minimum and maximum deflection angles, respectively.

FIG. 2B is a proposed SAW device 200 that does not include atransmissive optic 180. In the absence of a transmissive optic 180, thediffracted light 162-1 and 162-2 impinges upon distal face 168 at pointsA and B, respectfully. The diffracted light 162-1 and 162-2 are emittedfrom the distal face 168 as extremal rays of exit light 150-1 and 150-2.Here, the extremal rays of exit light 150-1/150-2 are simply given bySnell's law, as the rays traverse the interface between the refractiveindex of the substrate 120 (say, n˜2.3 for LiNbO3) to that of theambient medium 105.

FIG. 2C is a proposed SAW device 200 with the addition of thetransmissive optic 180, such as a chirped grating. The grating 180 islocated at the distal face 168. When diffracted light 162-1 and 162-2impinge upon points C and D of the grating 180, respectfully, extremalrays of exit light 150-1 and 150-2 are emitted. Here, the extremal raysof exit light 150-1 and 150-2 extend at angles, indicated by theta (θ),from nearly 90° in one direction to 90° in the other direction withrespect to the normal 111 to the substrate 120. Exemplary angle θ₂ forextremal ray of exit light 150-2 is shown.

In more detail, the remapping of the diffracted light 162 isaccomplished by rearranging the grating equation to obtain angle θ_(i)between each emergent ray of exit light 150 (in the first diffractionorder) and the normal 111:

$\theta_{i} = {\arcsin \left( {\frac{\lambda}{d} - \frac{\cos \mspace{14mu} \varphi_{i}}{n}} \right)}$

where n is the refractive index of the substrate 120, and use is made ofthe fact that the angle of incidence of a ray deflected toward thetransmissive optic 180 is the complement of its angle with respect tothe proximal face 160. As a well-known consequence of this equation, anypossible emergent ray angle can be created with a suitable choice ofspatial frequency of the grating 180 for a specified input angle.

A variation on the technique that has been described is to spatiallyvary the grating period (the reciprocal of the spatial frequency) alongthe extent of the grating 180. This spatial variation can be mapped tothe incoming deflection angle ϕ due to finite substrate propagationdisplacement. For example, the grating frequencies may be chosen so thatlight hitting the grating at the surface normal 111 is transmittedwithout additional deflection, whereas light striking the grating 180 atincreasingly oblique angles will experience greater and greaterdeflection. This deflection increases to the point where the maximumangle φ deflected by the surface acoustic wave 140 (for example +10°)will experience an additional deflection due to the exit-surface grating180, thereby experiencing a total deflection from the normal 111 at orapproaching 90°. The variation in angle θ provided by the grating 180for extremal (e.g. minimum and maximum) deflection angles φ₁ and φ₂ hastwo benefits: it may advantageously allow for the modest initialdeflection angles to be amplified, and it may advantageously suppressFresnel reflections, the undesirability of which has been discussedabove with reference to FIG. 1C.

A mirror or other reflective feature can be used to center the“deflection cone” of the surface acoustic wave 140, such that thecentral value is normal to the grating 180. This may provide symmetricdeflection.

A refinement to this technique is to tailor the grating 180 to workequally well at multiple wavelengths, such as red, green and blue (R, G,B) when used for visual display applications. Although R, G, B arereferenced here, all other ways of representing color may also be usedwithin the scope of the present invention. The grating may beconstructed through optimization to work over the entire color spectrumin one embodiment. This is accomplished through numerical optimization,with the starting point given by the grating equation. The gratinglayout is then optimized either through genetic algorithms or otherwell-known numerical methods to produce the highest efficiency and bestangular distribution. The actual spatial pattern will depend on thechoice of substrate material used for the SAW modulator 200, as well asthe maximum and minimum deflection of the surface acoustic wave 140, andthe material choice for the grating 180.

A grating in accordance with embodiments of the present invention may befabricated in any of the following ways, provided as examples andwithout limitation:

-   -   Etching directly into/onto the modulator wafer    -   Depositing metal dots or lines    -   Depositing dielectric dots or lines

Descriptions of exemplary genetic algorithms and numerical gratingoptimization techniques may be found in:

-   Zhou et al., “Genetic local search algorithm for optimization design    of diffractive optical elements,” Appl. Opt., vol. 38(20), pp.    4281-90 (1999);-   Lin et al., “Optimization of random diffraction gratings in    thin-film solar cells using genetic algorithms,” Solar Energy    Materials and Solar Cells, vol. 92(12), pp. 1689-96 (2008);-   Qing et al., “Crowding clustering genetic algorithm for multimodal    function optimization,” Appl. Soft Computing, vol. 8(1), pp. 88-95    (2008);-   Taillaert et al., “Compact efficient broadband grating coupler for    silicon-on-insulator waveguides,” Opt. Lett., vol. 29(23), pp.    2749-51 (2004);-   Shokooh-Saremi et al., “Particle swarm optimization and its    application to the design of diffraction grating filters,” Opt.    Lett., vol. 32(8), pp. 894-96 (2007); and-   Byrnes et al., “Designing large, high-efficiency,    high-numerical-aperture, transmissive meta-lenses for visible    light.” Opt. Exp. 24 (5), pp. 5110-5124 (2016).

FIG. 3 depicts an example of reflected diffracted light 162′ incidentupon a transmissive optic 180 such as a grating of a proposed SAW device200. As shown, the deflection is symmetrical about the point x₂, whichis normal of the exit distal face 168, and the spatial spread of thedeflection angle ϕ is approximately equal to x.

As in FIGS. 2A and 2B, φ₁ and φ₂ are the minimum and maximum deflectionangles possible for the diffracted light 162. The diffracted light 162reflects off end face 170 as reflected diffracted light 162′. Here, theedge cut angle β of the end face 170 is typically chosen such that adeflection of at least half of the available cone of the deflectionangle φ, or φ/2, is normal or near normal to the distal face 168.

Spatial  Spread    (=)x $\begin{matrix}{\left. {{{So}\mspace{14mu} {Deflection}} = {\frac{\phi}{2} =}} \right)\mspace{14mu} {normal}} \\{\left. {= {0 =}} \right) - \frac{\phi}{2}} \\{\left. {= {\phi =}} \right)\frac{\phi}{2}}\end{matrix}$

FIG. 4 is a plot of the spatial frequency of the grating 180 shown inFIG. 3 as function of position. As shown, the amount of deflection issymmetric with respect to the distance defined by x (i.e. the size ofthe grating) in one example. This symmetry is not required in allembodiments of this invention, but is merely illustrative, however.

FIG. 4 is a plot of the spatial frequency for three embodiments of thegrating 180 shown in FIG. 3 as function of position. As shown, theamount of deflection is different at different locations within thegrating.

Due to finite substrate propagation displacement, different initialdeflection angles φ will experience the varying spatial frequencies asdepicted in FIG. 4. Thus, more deflection of the diffracted light 162will occur when the light reaches the grating 180 proximate to pointsx1, while less deflection will occur at the proximate to the point x3when the grating is constructed with a spatial frequency according tocurve A. The result is an increase in the angular fan of the exit angleα of the exit light 150 beyond that created by initial interaction ofthe guided light 301 with the surface acoustic wave 140.

On the other hand, when the grating is constructed with a spatialfrequency according to curve C, more deflection of the diffracted light162 will occur when the light reaches the grating 180 proximate topoints x3, while less deflection will occur at the proximate to thepoint x1.

On the other hand, when the grating is constructed with a spatialfrequency according to curve B, more deflection of the diffracted light162 will occur when the light reaches the grating 180 proximate topoints x1 and x3, while less deflection will occur at the proximate tothe point x2, at the center of the grating.

A second family of techniques to increase the angular extent of the exitangle α of the fan of exit light 150 is to use geometrical opticaltechniques, i.e. adding or “hollowing-out” diverging optical featureson, or near, the SAW modulator 200. These features may be used toincrease or decrease the optical power to optimize the fan of the outputlight.

It should be understood by one of ordinary skill in the art that thevarious described techniques of creating a refractive lens at anoutput/exit face, and adding optical power to the system may be doneusing hybrid diffractive-refractive optics. Such optical systems aregenerally known to those of ordinary skill in the art and can be foundin Stone et al., “Hybrid diffractive-refractive lenses and achromats,”Appl. Opt., vol. 27(14), pp. 2960-71 (1988).

FIG. 5A is an illustrative example for yet another transmissive optic180. Here, the optic 180 is formed by removing material from the lithiumniobate substrate 120 at the distal face 168 as an exit face to create aconcave optical surface 180. The curved optical surface 180 providesdiverging optical power, thereby broadening the angular extent of theexit angle α of the fan of exit light 150. In other examples, opticalelements that provide the optical power might be placed upon an exitface, patterned flat on a surface such as an exit face, and included aspart of a later optical train.

In more detail, the guided light 301 is diffracted from the waveguide102 by the surface acoustic wave 140 and propagates through thesubstrate 120 as diffracted light 162. In the illustrated embodiment,this diffracted light 162 is reflected by the end face 170 as reflecteddiffracted light 162′. As shown, the distal face 168 is made (e.g.patterned) to have a concave optical surface 180 to provide opticalpower to the wave of reflected diffracted light 162′, thus expanding thedivergent nature of the light wave. The light wave 162′ can theninteract with the optical surface 180 to diverge, further creating anexit angle α of greater than 90 degrees.

Due to imperfections in the substrate 120 and differences between theindices of refraction of substrate 120 and ambient medium 105, some ofthe diffracted light 162 might exit the SAW device 200 as unwanted strayexit light 174 from end face 170. In one example, an opaque layer may beapplied to the end face 170 to minimize or eliminate the stray exitlight 174.

FIG. 5B is another example of the transmissive optic 180. Here, theoptic 180 is formed by adding material to the lithium niobate substrate120 at the distal face 168 as an exit face to create a convex opticalsurface 180.

FIG. 6 shows a ray trace illustrating the propagation of light in theembodiment of the SAW device in FIG. 5. The diffracted light 162propagates toward the end face 170. This reflects the light 162 asreflected diffracted light 162′. This light 162′ then interacts with thetransmissive optic 180, which in the illustrated embodiment is a concaveoptical surface. Other embodiments of the present invention in which thesubtense of the exit angle α of the fan of exit light 150 for a SAWmodulator 200 might be enhanced are now described with reference toFIGS. 6B and 7A-7N.

The following table describes each of the ray traces in FIG. 7A-7N. Eachrow/entry in the table describes a separate ray trace FIG. 7A-7N. Fieldswithin each row includes typical values for the internal deflectionangle φ and edge cut angle β, and resulting output angular subtense α. A“comments” field is also included. More detail for each of the ray traceFIGS. 7A-7N accompanies the descriptions of these figures, providedherein below.

Approx. Output Edge Exit angle Internal Cut fan or Angle Angle SubtenseFig. (ϕ°) (β°) (α°) Comments 7A 10  90 25 Base case, showing one smallactive area as possible subset of grating. Diffractive structure on topface (e.g., SAW or other grating). Right-angle edge face. 7B 10  90Varies Base case, illustrating diffractive fan as modulated by threeregions along, e.g., a SAW. 7C 10  40 40 Exits face opposite modulatorchannel. Grazing beam exits approximately normal to exit face. 7D 10  5035 Exits face opposite modulator channel. Edge cut to position mediandiffracted ray normal to output. 7E 10  52 33 Exits face oppositemodulator channel. Edge cut to position maximally diffmcted ray to exitnormal. 7F 10  60 ~60  Exits face opposite modulator channel. Edge cutso that grazing ray just misses total internal reflection (TIR) at exitface. 7G 10  63 N/A Edge cut so that grazing ray just avoids TIR, andexits the edge face. 7H 10  80 ~35  Edge cut so that themaximally-diffracted ray just misses TIR and exits nearly gmzing to theoutput edge. 71 10 100 30 Exits edge. Edge cut to make centraldiffracted ray exit normal to edge face. 7J 10 120 (example) Exits edge.Edge cut such that grazing input ray just missed TIR condition. 7K 20<90 ~90  Exits edge. Diffraction period and edge angle chosen such (89)that the output subtends approximately 90 degrees. 7L 20 105 50 Exitsedge. Median ray exits normal to exit face. 7M 20 140 (example)Single-reflection TIR. Fan exits same face as diffracting structure(SAW). 7N 20 160 (example) Double-reflection TIR. Fan exits edge face.

It is to be understood that, within the scope of certain embodiments ofthe present invention, that the various faces may serve as the exitface, either with an intervening reflection at a face or without. It isalso to be understood that the length of the SAW modulator 200 and/orthe proximal face 160 and/or distal face 168 may be varied within thescope of the present invention. Additionally, either end face 170 and/ordistal face 168 may be cleaved and/or polished or otherwise angled,within the scope of the present invention. For example, the wafercontaining the SAW devices 200 may be lapped at an angle. All techniquesfor fabricating a SAW modulator 200 with faces at non orthogonal anglesare within the scope of the present invention. Also, the interactionregion (the places where the SAW and the light interact and kick out theleaky mode light) has a finite extent, e.g. 4 mm, 8 mm. A consequence ofthis, the values the exit angle fan or subtense are generallyapproximations.

Ray traces are shown, by way of example only, for a variety ofgeometrical configurations of SAW modulator 200 in FIGS. 7A-7N, and areby no means intended to limit the application of the principles taughtherein. FIGS. 7A-7N assume the absence of an anti-reflective (AR)coating. However, the effect of such an AR coating can be readilycalculated, given the indices of refraction of substrate 120 and ambientmedium 105. The AR coating would typically be applied, insofar as an ARcoating is beneficial, as elsewhere discussed herein.

FIG. 7A is a base ray trace example, in accordance with the prior art.End face 170 is at a 90° edge cut angle β with respect to the proximalface 160. A typical value for the deflection angle φ is 10°. Here, thediffracted light 162 exits near orthogonal to end face 170 as exit light150.

FIGS. 7B-7N depict exemplary ray traces in proposed SAW devices 200constructed according to embodiments of the present invention.

FIG. 7B illustrates a fan of exit light 150 that is diffracted atregions 190, 192, 194. There is a finite interaction region along whichthe waveguided light interacts with the SAW to become leaky-mode light.This illustrates an interaction region from 190 to 194, with anintermediate point 192 shown. If a single-frequency RF signal drives theIDT, there is essentially one “ray” emitted at each of 190, 192, and194, and at intermediate points. This “fills” the output face in thisillustration. As in FIG. 7A, the end face 170 is at a 90° edge cut angleβ with respect to the proximal face 160. A typical value for thedeflection angle φ is 10°. Here, the exit angle fan α is defined asapproximately the maximum subtense of the steered light, in air andvaries due to the modulation.

FIG. 7C-7H are ray traces for SAW devices 200 having an acute edge cutangle β. In each of FIG. 7C-7H, a typical value for the deflection angleφ is 10°.

FIG. 7C shows a ray trace in which the diffracted light 162 reflects offof the end face 170 as reflected diffracted light 162′. This end face170 has an edge cut angle β of about 40°. Then, the reflected diffractedlight 162′ propagates through the substrate 120 towards the distal face168, which functions as the exit face. The reflected diffracted light162′ exits the SAW device 200 as exit light 150, approximately normal tothe distal face 168. Here, an exemplary value for the exit angle fan αis as high as 40°.

FIG. 7D shows a similar configuration as in FIG. 7C. The diffractedlight 162 reflects off the end face 170 as reflected diffracted light162′. Here, however, the end face 170 is at a greater edge cut angle βto the proximal face 160, such as about 50°. This has the effect ofchanging the general direction of the exit light 150 with respect to thedistal face 168. Specifically, the end face 170 is edge cut to positionmedian diffracted rays of the reflected diffracted light 162′ to benormal to the distal face 168 as the exit face. The reflected diffractedlight 162′ is transmitted out the distal face 168 as exit light 150.Here, an exemplary value for the exit angle α is as high as 35°.

FIG. 7E shows a similar configuration as in FIG. 7D. Here, however, theexit face 170 is at a greater edge cut angle β to the proximal face 160,such as about 52°. This has the effect of further changing the generaldirection of the exit light 150. Specifically, the end face 170 is edgecut to position maximally diffracted rays of the reflected diffractedlight 162′ to be normal to the distal face 170 as the exit face. Here,an exemplary value for the exit angle fan α is as high as 33°.

FIG. 7F shows a similar configuration as in FIG. 7E. Here, however, theend face 170 is at a still greater edge cut angle β to the proximal face160, such as about 60°. This has the effect of further changing thegeneral direction of the exit light 150. Specifically, the end face 170is edge cut so that grazing rays of the reflected diffracted light 162′just miss being totally internally reflected (TIR) at the end face 170,but instead are emitted near the Brewster angle, thus minimizingundesirable Fresnel reflections. The reflected diffracted light 162′exits the SAW device 200 at distal face 168 as exit light 150,approximately normal to the distal face 168. Here, an exemplary valuefor the exit angle α is approximately 60°. Also shown is a Fresnelreflected component 164 arising at the distal face 168.

The Fresnel reflected component 164 can be addressed. In one example,this component is preferably minimized by adding an AR coating to thedistal face 168 to minimize or possibly eliminate the Fresnel reflectedcomponent 164.

FIG. 7G shows a similar configuration as in FIG. 7F. Here, however, theend face 170 is at a greater edge cut angle β to the proximal face 160,such as about 63°. This has multiple effects. First, not all of thediffracted light 162 is transmitted out the end face 170 as exit light150. Rather, some of the diffracted light 162 is reflected internally asstray internally reflected light 172. Second, when the stray internallyreflected light 172 impinges on the distal face 168, the strayinternally reflected light 172 is totally internally reflected.

The stray internally reflected light 172 can also be corrected. In oneexample, an antireflective (AR) coating might be applied to the exitface (here, end face 168) to minimize or possibly eliminate the strayinternally reflected light 172. Further, an absorber material should beadded to the distal face 168 to absorb light reflected light and preventfurther stray light reflections.

FIG. 7H shows a similar configuration as in FIG. 7G. Here, however, theexit face 170 is at a greater edge cut angle β to the proximal face 160,approaching 80°. As in FIG. 7G, some of the diffracted beam 162 isreflected internally as stray internally reflected light 172 and istotally internally reflected at the distal face 168. Here, an exemplaryvalue for the exit angle fan α is approximately 35°.

FIGS. 7I-7N are described below and show various combinations ofinternal reflections and exit angles α for additional edge cut SAWdevices 200. In this group of figures, with the exception of FIG. 7K,the edge cut angle β is obtuse.

In more detail, in FIG. 7I, the end face 170 is edge cut to makecentrally diffracted light 162 exit normal to the end face 170 as exitlight 150. Some of the diffracted light 162 might also be reflectedinternally as stray internally reflected light 172. The edge cut angle βis about 100° and provides an exit angle α of approximately 30°. Atypical value for the deflection angle φ is 10°.

In FIG. 7J, the end face 170 is edge cut such that grazing input raysjust miss the TIR condition at the end face 170. The diffracted light162 exits the end face 170 as exit light 150. The edge cut angle isabout 120° and the exit angle α varies, as shown.

In FIG. 7K, the diffraction period and edge cut angle β are chosen suchthat the exit angle α is approximately 90 degrees. The diffracted light162 exits the end face 170 as exit light 150. Here, the edge cut angle βis typically less than 90° (a value of 89° was selected here). A typicalvalue for the deflection angle φ is 20°.

According to FIG. 7L, median rays of the diffracted light 162 exitsnormal to the end face 170 as exit light 150. Here, the edge cut angle βis 105° and the output angular subtense α is typically 50°. A typicalvalue for the deflection angle φ is 20°.

In FIG. 7M, a single-reflection-TIR case is shown. The diffracted light162 exits as exit light 150 from the same exit face (here, proximal face160) as the SAW propagates along. Here, the edge cut angle β is 140°.Unwanted stray exit light 174 is also transmitted out of end face 170. Atypical value for the deflection angle φ is 20°.

FIG. 7N shows a double-reflection TIR case. The diffracted light 162exits the edge face 170 as exit light 150. Here, the edge cut angle β is160°. Unwanted stray exit light 174 is also transmitted out of proximalface 160. A typical value for the deflection angle φ is 20°.

It is to be understood that antireflective (AR) coatings are preferredat the exit faces of the SAW modulator 200, given the Fresnelreflections due to the typically large discontinuity of index ofrefraction between substrate 120 and the ambient medium 105. The designof antireflective coatings for the spectral and angular ranges involvedhere is well within the capabilities of a person of ordinary skill inthe art, as is calculating the effect of coating the face on theemerging fan. All antireflective coating techniques are within the scopeof the present invention.

When assembled into a display operating in a horizontal-parallax-onlymode (i.e. the diffracted fans steer horizontally), it is often alsodesirable to spread the beams of diffracted light 162/reflecteddiffracted light 162′ vertically. This is typically done with a verticaldiffuser. Such methods may be applied, within the scope of the presentinvention, to all of the embodiments discussed above. Moreover, all ofthe foregoing teachings may also be applied for vertical displacement.Thus, if the beams 162/162′ exit the narrow edge of exit face 170, thenarrow edge may be augmented with a transmissive optic 180, such as alens or a grating, as taught above, to further condition the exit light150.

Electro-Holographic Light Field Generator Device Architecture

FIG. 8A shows a proximal face 160, FIG. 8B shows a distal/exit face 168,and FIG. 8C shows a side cross-sectional view (all not to scale) of anelectro-holographic light field generator device 300 according to anembodiment of the present invention.

In general, the electro-holographic light field generator device 300comprises an array of SAW devices or modulators 200. These SAW devices200 are fabricated in a common substrate 120. As best shown in FIG. 8A,the longitudinal axes of each of these SAW devices 200 extend parallelto each other across the light field generator device 300 in the x-axisdirection. Note: the axes x, y, z are used here to orient the geometryof the light field generator system and its components for clarity. Thiscoordinate system has no relation to the x,y,z crystallographic axes oflithium niobate or any other material.

In more detail, and as described hereinabove, the substrate 120 may bemade, for example, of lithium niobate following known processes such asthat disclosed in Smalley. Many other materials and design choices areavailable including other piezoelectric materials and crystallographicorientations, and waveguide architectures such as planar, ridge, rib,embedded, immersed, and bulged. Doping such as MgO-doped lithium niobatemay be useful, in some cases.

The array of surface acoustic wave (SAW) optical modulators 200 isarranged in the y-axis direction across the width of the commonsubstrate 120. Each SAW optical modulator 200 includes an in-couplingdevice 106 (e.g., a laser in-coupling grating or prism), a waveguide 102and a SAW transducer 110 (e.g., an IDT, for example).

As described before, the waveguides 102 provide confinement of the inputlight in a TE (transverse electric) guided mode 301, in one example. TheSAW transducers 110 are driven by an RF input signal 130 that creates acorresponding surface acoustic wave 140 that propagates collinearly withthe light 301 in the waveguide 102 and which interacts with the light toconvert part of the light to the transverse magnetic (TM) polarization,leaky mode.

Birefringence of the waveguide 102 and the optical substrate 120 (and/orthe wave-vector change from the interaction) causes the TM leaky modeportion of the light propagating in the waveguide 102 to leak out of thewaveguide 102 into the optical substrate 120 as diffracted light 162towards the exit face, which is the distal face 168, in this embodiment.

In different embodiments, the IDTs 110 can occupy a variety of specificlocations and specific orientations with respect to the waveguide 102.For example, in the illustrated embodiment, the transducers 110 arelocated near the end face 170 so that the surface acoustic waves 140will propagate in a direction opposite the propagation of the light inthe waveguides 102. In other embodiments, however, the transducers 110are located near the in-coupling devices 106 so that the surfaceacoustic waves 140 will co-propagate in the direction of the light inthe waveguides 102.

Also, there could be multiple SAW transducers 110 for each in-couplingdevice 106/waveguide 102, with each SAW transducer 110 responsible for adifferent specific bandwidth around a given center frequency (e.g.:100-150 MHz, 150-250 MHz, and 250-400 MHz).

In a specific embodiment, the array of SAW optical modulators 200 may bepacked relatively tightly with a waveguide separation 206 of between 10μm-400 μm, for example, 50 μm. The waveguide length 207 may be 1-10centimeters (e.g., 5 cm) or even longer if multiple SAW transducers 110and/or multiple laser inputs 106 are used to mitigate acoustic andoptical attenuation respectively. In this context, a greater waveguidelength 207 reduces system complexity and, if tiled into a largerdisplay, it minimizes tile-borders (“grout”). Since the surface acousticwaves 140 move at the speed of sound, the light inputs 101 may bestrobed at a repetition rate equal to or lower than the inverse acoustictransit time, at a pulse width sufficiently narrow (for example, in therange of nanoseconds to microseconds) to cause acceptably low blurring.

Each waveguide 102 may be configured for a single specific wavelength ofinput light 101, which in this context should be understood to includeat least one of visible light, infrared light and ultraviolet light, orfor multiple different light wavelengths. For example, for 3D displayapplications, each waveguide 102 may carry one or more of red, green, orblue light 101. In other specific light field generation applications,other wavelength combinations may be useful including more or fewer thanthree colors and/or non-visible wavelengths.

FIG. 8B shows the distal face 168 of a light field generator device 300,which is the exit face in the illustrated embodiment. According to theembodiment, the optical substrate 160 includes a two dimensional array310 of output optics 303 for shaping output exit light 150. Inillustrated example, the exit light 150 is collimated into a beam,focused at infinity.

The output optics 303 are diffractive lenses arranged into lens strips302 (e.g., one strip for each waveguide). Each of the strips 302 isaligned under a respective waveguide 102. Each individual output optic303 is the length of a display pixel (100 μm-2 mm, typically about 1 mmin the x-axis direction). Thus, with a waveguide pitch 206 of 50 μm eachdiffractive lens output optic 303 would be 1 mm×50 μm, and eachdiffractive lens strip 302 may be about 5 cm×50 μm.

The diffractive lens strips 302 may be chirped gratings with componentsthat redirect light in both directions. That is, rectangular sections ofa diffractive lens, which may or may not have different focal lengths inthe horizontal and vertical directions, where “horizontal” meansparallel to the length of the respective waveguide 102 (x-axisdirection) and “vertical” means across the width of the respectivewaveguide 102 (y-axis direction).

Diffractive lens output optics 303 may be fabricated, for example andwithout limitation, by etching directly into/onto the substrate 120,depositing metal dots or lines, or depositing dielectric dots or linesor pillars. Descriptions of exemplary generic algorithms and numericalgrating optimization techniques may be found in:

-   Zhou et al., Genetic local search algorithm for optimization design    of diffractive optical elements, Appl. Opt., vol. 38(20), pp.    4281-90 (1999);-   Lin et al., Optimization of random diffraction gratings in thin-film    solar cells using genetic algorithms, Solar Energy Materials and    Solar Cells, vol. 92(12), pp. 1689-96 (2008);-   Qing et al., Crowding clustering genetic algorithm for multimodal    function optimization, Appl. Soft Computing, vol. 8(1), pp. 88-95    (2008);-   Taillaert et al., Compact efficient broadband grating coupler for    silicon-on-insulator waveguides, Opt. Lett., vol. 29(23), pp.    2749-51 (2004);-   Shokooh-Saremi et al., Particle swarm optimization and its    application to the design of diffraction grating filters, Opt.    Lett., vol. 32(8), pp. 894-96 (2007); and-   Byrnes et al., Designing large, high-efficiency,    high-numerical-aperture, transmissive meta-lenses for visible light,    Opt. Exp. 24 (5), pp. 5110-5124 (2016).

The surface acoustic wave (SAW) optical modulators 200 on the proximalface 160 and the two dimensional array 310 of output optics 303 on thedistal face 168 need to be carefully aligned in the width (y-axis)direction so that each waveguide 102 sends light into its correspondingdiffractive lens strip 302. Their alignment in the longitudinaldirection (x-axis) is less critical because it can be corrected for inthe operating software during a calibration step in which a waferthickness profile (including thickness non-uniformity) also can bemeasured and corrected.

FIG. 8C is a schematic cross-section of a light field generator device300, showing a SAW modulator 200 constructed with diverging diffractivelens output optics 303.

An RF controller 405 includes at least one hardware implementedprocessor device that is controlled by software instructions totranslate a desired 3D image into an appropriate RF waveform to controlthe respective SAW optical modulators 200 of the electro-holographiclight field generator device 300. The objective is to develop the exitlight 150 produced from all of the modulators 200 of the light fieldgenerator device 300 as a three-dimensional output light field. Softwarefor driving electro-holographic displays of a variety of forms isdescribed, for example, in Mark Lucente, Computational holographicbandwidth compression, IBM Systems Journal, 35(3 & 4), 349-365 (1996);Quinn et al., Interactive holographic stereograms with accommodationcues, Practical Holography XXIV: Materials and Applications, ed. Hans I.Bjelkhagen and Raymond K. Kostuk, SPIE (2010); and Jolly et al.,Computation of Fresnel holograms and diffraction-specific coherentpanoramagrams for full-color holographic displays based on leaky-modemodulators, Proc. SPIE Practical Holography XXIX, 9386, 93860A (Mar. 10,2016).

The resulting three-dimensional output light field is similar tointegral photography 3D displays in which there are known algorithms fordeciding how much light to put into which views of which pixels. Suchintegral photography algorithms are usable in this context, or they canbe modified for even better performance, for example, by adding inaspects of algorithms for electro-holographic display such as how tochoose and adjust wavefront curvature (See, e.g., Smithwick et al.,Interactive holographic stereograms with accommodation cues, PracticalHolography XXIV: Materials and Applications, ed. Hans I. Bjelkhagen andRaymond K. Kostuk, SPIE (2010)). Another algorithm improvement is thatthe number of views that can be calculated and projected can bedetermined and updated in software to optimize the display qualityrather than being fixed in hardware. In addition, the view direction canbe continuously adjustable in one dimension.

Once the RF controller 405 determines how much light 101 needs to be putinto a given view of a given pixel, the RF controller 405 thendetermines what waveforms of the RF drive signals 130 need to be appliedto the transducers 110 of the respective SAW optical modulators 200 toproduce that outcome. This involves determining the appropriate outputoptics 303 to use—each output optic 303 is able to send light of aparticular wavelength into any of typically 10-100 differentnon-overlapping views.

Once the appropriate output optics 303 are determined, the RF controller405 executes a computational back-propagation of that light through theoutput optics 303 and back into the corresponding waveguide 102. Thecomputational interference between that back-propagated light and thewaveguided light finally determines a specific waveform of the surfaceacoustic wave 140 to be used. In specific embodiments, theback-propagation can be pre-computed into a lookup table. For example,to create an approximately-collimated beam of exit light 150 (focused atinfinity), a given specific chirped RF waveform creates a correspondingsurface acoustic wave 140 in the waveguide 102, which createsout-coupled diffracted light 162 as shown in FIG. 8C. This diffractedlight 162 approximately converges towards a certain point on thehorizontal focal plane 404 of the diffractive lens output optic 303(either in front of or behind the output optic 303 depending on whetherthe lens of the output optic 303 is diverging (as shown in FIG. 8C) orconverging (as shown in FIG. 9 discussed below).

In the specific embodiment shown in FIG. 8C, each diffractive lensoutput optic 303 has the same length as an output pixel and spreads theradiated exit light 150 into a desirable field-of-view in the horizontaldirection, for example, 90°. This information, together with the RFbandwidth and substrate index of refraction of the substrate 120 all areassociated with a chirped spatial frequency profile of the diffractivelens output optic 303 and the diffractive lens strips 302 (which againacts as a slice of a diffractive lens in this specific embodiment).

It should be understood that in this context there is not some specificunique output optic 303 geometry that is optimal for a desiredfield-of-view. Rather there are multiple possible nominally acceptabledesigns with different characteristics such as different focal lengths,different lens centers, and/or specific optical aberrations. Forexample, some designs may be sharpest in the center of the field ofview, while others are sharper towards the sides of the field-of-viewbut blurrier in the center. Selection of a specific profile for theoutput optics 303 is a matter of design choice.

Thus the RF controller 405 is configured to develop a hybridthree-dimensional output light field formed from the exit light 150transmitted by SAW devices 200 of the light field generator devices 300.The output light field is holographic horizontally andspatially-multiplexed horizontally, vertically, or both to improve theangular range or resolution horizontally, vertically, or both, and alsoto incorporate the three colors. In the vertical direction, eachdiffractive lens output optic 303 can collimate (or approximatelycollimate as desired) the leaky mode diffracted portion of the waveguidelight 162 coming out of the respective waveguide 102 and send it into aspecific uniform vertical direction. With 50 μm-spaced (see reference206) waveguides 102 and 1 mm× 1 mm pixel size, then ˜7 differentvertical views may be produced, 7×3×50 μm≈1 mm (where the 3 is tosupport red, green, and blue). The horizontal views can be continuouslyadjusted though there is a limit caused by the extent to which theradiation output 150 can be horizontally collimated; i.e. the blurrinessof the horizontal view direction. The number ofnot-substantially-overlapping horizontal views may be in the 10-100range, and depends on the RF bandwidth driving the SAW opticalmodulators 200.

A specific embodiment may utilize horizontal spatial multiplexing byputting two or more output optics 303 horizontally within each displaypixel 304, in order to trade-off between the number of vertical viewsand horizontal views. The diffractive lens output optics 303 areoptimized for maximum efficiency, so they should have anti-reflectiveproperties.

Within each display pixel 304, the waveguides 102 can be arranged in ablocked order (e.g. RRRRGGGGBBBB) or in an interleaved configuration(e.g. RGBRGBRGBRGB). In blocked order, the diffractive lens outputoptics 303 may be configured such that vertically-neighboring outputoptics 303 merge into each other and are combined together into largerdiffractive lens structures 304 (e.g., larger rectangular sections cutout of a single diffractive lens). This can help mitigate the issue whensome light from a waveguide 102 travels vertically (in the y-axisdirection in the Figures) and hits an unintended output optic 303.Interleaved order could also help with this same issue in a differentway, if the diffractive lens output optics 303 respond in a narrow-bandway and reject the light from an unintended neighboring waveguide 102.Blocked order may also make the optical layout (laser in-couplingconfiguration) simpler.

Depending on the specific application, the in-coupling device 106 candeliver the input light 101 into the waveguides 102 from eitherdirection, in some cases simultaneously, but more often with interleavedstrobes so that each optical direction obtains its own RF waveform. Thiscould double the number of views per RF bandwidth. For example, we canhave one laser direction send light into the left half of thefield-of-view, and the other into the right half—one light input 106would diffract off the +1 grating order and the other (co-located withSAW transducers 110) off the −1 grating order of the same diffractivelens output optic 303.

The waveguides 102 can carry red, green, and blue light eithersimultaneously or in interleaved strobes. The diffractive lens outputoptics 303 can be optimized for broadband and/or to impart phaseindependently for the three colors (e.g. Aieta et al., Multiwavelengthachromatic metasurfaces by dispersive phase compensation, Science 347,1342 (2015), which is incorporated herein by reference in its entirety).

FIG. 9 shows a side cross-sectional view of an alternate embodiment forone of the SAW modulators 200 of an electro-holographic light fieldgenerator 300 in which the diffractive lens output optics 303 areconverging, rather than diverging as in FIG. 8C. In this embodiment, theleaky mode diffracted light 162 from the waveguides 102 is modulated bythe surface acoustic waves 140 to converge at a focal plane 404 withinthe substrate 120 so that it is diverging as it enters an output optic303. The output optic 303 then converges the radiated exit light 150into a collimated beam (focused at infinity).

FIG. 10 shows a side cross-sectional view of an alternate mode ofoperation for an electro-holographic light field generator 300. In thismode, the RF controller 405 operates the SAW optical modulators 200 sothat the leaky mode diffracted light 162 passing through the outputoptics 303 converges towards a virtual focus 601 above the focal plane404 of a lens output optic 303 by controlling the RF drive waveform. Asa result, the radiated exit light 150 from each output optic 303 has aselected output focal point 603 beyond the focal plane 404 before thelocation of the observer. The surface acoustic wave 140 can becontrolled to locate the output focal point 603 at any desired specificdistance (within reasonable limits).

In some embodiments, the output optics 303 may be reflective rather thantransmissive, e.g. as a curved mirror or as a reflective diffractivelens. This could entail some modification of the grating period profileand/or an anti-reflective coating on the surface of the wafer throughwhich the light enters the air. This surface may be the waveguidesurface, or may be an edge.

The diffractive lens periodicity profile may not specifically be asection of a conventional diffractive lens, but may be modified—forexample, including some positive or negative spherical aberration—inorder to optimize the distribution, blurriness, wavefront curvature(focus), and other properties of the views. For the same reason, the RFencoding may be more complicated than described in the embodimentsdescribed above, and more specifically may be modified from theback-propagation algorithm results, for example by apodization of the RFwaveform in the time or frequency domain. The diffractive lens outputoptics may have a helical property such that horizontal positiondetermines vertical deflection, instead of (or in addition to)horizontal deflection. In such a case, the display may usefully beoriented with vertical rather than horizontal diffractive lenses.

FIG. 11A shows a side cross-sectional view of anotherelectro-holographic light field generator 300. A SAW device 200 withinthe light field generator 200 is shown, in which the end face 170functions as the exit face. Thus, the exit face need not necessarily bethe distal face 168. A single output optic 303 is at the distal face168. In this example, the RF controller 405 operates the SAW opticalmodulators 200 so that the leaky mode portion of the diffracted light162 converges towards a focal point 603 beyond the side exit surface/endface 170, which is deflected by the output optic 303 as a side radiatedexit light 150. The output optic is a refractive lens or diffractivelens/grating in different examples.

By using a variety of different focal depths per pixel, a displayconstructed from the light field generators 200 can be improved inseveral metrics including image quality and depth,vergence-accommodation conflict, and astigmatism. In the horizontal(x-axis) direction, the operating software can accomplish that by usingan RF encoding to the SAW optical modulators 200 that sends lighttowards a point in front of or behind the diffractive lens focal plane.In the vertical (y-axis) direction, the diffractive lens output optics303 can have different focal lengths in different areas of the substrate120. The feature of continuously-adjustable view direction (as opposedto discrete views) can be helpful for display quality, particularlyalleviating some aliasing issues common with other 3D displays (e.g.Zwicker et al., Antialiasing for Automultiscopic 3D Displays,Eurographics Symposium on Rendering, 2006). This is somewhat related toability to manipulate wavefront curvature as described above, whichsimilarly helps improve display quality.

The approaches described above enable a higher display quality due tothe small effective (sub) pixel size, lack of horizontal aliasing, andability to continuously adjust the horizontal wavefront curvature. Theconventional acousto-optic-modulator-based holographic 3D display (e.g.“MIT Mark 1”, 2, or 3) is horizontal-parallax-only (HPO) made with anacousto-optic or SAW modulator in a descanning configuration (e.g. witha spinning polygon). But such descanning is very challenging at best ina thin display with no-moving-parts. Descanning can be avoided usingstrobe lights (e.g. Jolly et al., Near-to-eye electroholography viaguided-wave acousto-optics for augmented reality, Proc. of SPIE Vol.10127, 2017), but the thin form factor also prevents overalldemagnification and hence leads to a very limited angle exit fan.

There are some known ways to increase the angle fan in anelectro-holographic display without pixelating the holo-line asdescribed above, but no one has previously suggested breaking theholo-line into pixels and using lenses to increase the angle spread ofeach pixel. Of course, this is not a conventional holographic technique,but is more like a hybrid with integral photography. Cutting up thehologram as described above does reduce the image quality compared to afull proper hologram, but degradation is likely to be acceptable in manypractical applications and certainly can be better than non-holographicalternatives.

The combined configuration of the lens focal plane 404, waveguide 102,and RF encoding such as that shown in FIG. 8C is particularly beneficialover known conventional approaches to encoding the discrete data (whichviews of which pixels should be turned on in each video display frame)into an RF waveform such as encoding the data-points in differenttime-slots or in different frequency-slots in the waveform. Rather, eachdata point contributes a specific chirped waveform spread out in bothtime and frequency, which greatly increases flexibility as to thelocation and orientation of the diffractive lens array. That allows theuse of a flat pattern on the back side of a wafer-shaped opticalsubstrate, which can be very convenient in practice.

In some embodiments, it may be useful to have a second layer ofdiffractive lenses or other optical components, for example, to dealwith diffraction effects. In addition or alternatively, the transmissivediffractive lenses can be replaced or supplemented by refractive orreflective optics; e.g., either cut out of the optical substrate 102 orattached to the optical substrate. Some embodiments may also omit thevertical parallax response, instead making a horizontal-parallax-only(HPO) display. Such a display may be simpler to implement with fewerwaveguides, which can be larger and spaced farther apart, which in turnmay make the system easier to build for various reasons, includingreducing the number of RF and optical connections, switches, anddrivers.

FIG. 11B is another implementation of the electro-holographic lightfield generator 300 in FIG. 11B. Here, two output optics 303 provided onend face 170.

In some embodiments, it may be useful to maximize thinning of theoptical substrate 120 to reduce the distance between the waveguide layerand diffractive lens output layer. In some instances, this gap may needto be so thin that these two components cannot be on two opposite sidesof a single self-supporting wafer.

FIG. 12 illustrates one possible process of creating a substrate 120that minimizes component separation.

In step 1, a piezoelectric material wafer 410 and a support substrate(e.g. glass) are selected. In one example, the piezoelectric material islithium niobate.

In step 2, the piezoelectric material is planarized and then patternedwith output optics such as a two dimensional array 310 of output optics303 and described previously.

The piezoelectric material wafer 410 is then bonded to the separatesupport substrate or wafer 412 using a wafer bonding process in step 3.This encapsulates the output optic array 310 between the two wafers orsubstrates.

Then, the piezoelectric material wafer 410 is mechanically thinned downin step 4 to produce final thickness for the device substrate 120. Thiscan be performed using CMP, for example. CMP is chemical mechanicalpolishing/planarization, which thins and smooths the surface of thewafer using a combination of chemical and mechanical forces.

According to step 5, topside components 414, such as waveguides 102,incoupling devices 106, and IDTs 110, are patterned within/upon thesurface of the now-thinned piezoelectric material 410 which willfunction as substrate 120. If a second layer of diffractive lenses ormicro-lenses is needed, it can be provided on the back of thepiezoelectric material 410 as layer 414, or the back of the substratecould be made reflective, enabling two passes through the output optics.As with other surfaces, the back of the substrate could also have ananti-reflective coating.

FIG. 13A illustrates time-multiplexing of input light 101 and/or RFinput signals 130 applied to a light field generator device 300. Thelight field generator device 300 includes an array of SAW devices 200.

One challenge of SAW-based electro-holographic displays is the largenumber of illumination in-coupling ports 106 and RF drive lines 130. Thepresent embodiment addresses the issue of coupling light into each ofthe waveguides 102 by relying on time-multiplexing.

As before, the proximal face 160 includes an array of waveguides 102.These multiple waveguides 102 are fed with an optical signal input lightsource 902 using beam displacer 905. The input light source 902 providesone or more wavelengths of input light 101, such as red, green and blue.In one example, the input light source 902 is a laser or system oflasers.

The beam displacer 905 operates via any of several techniques forsteering or displacing the laser beam of input light 101 into thewaveguides 102-1 to 102-N (e.g., liquid crystal steering (as in SR Daviset al., Analog, non-mechanical beam-steerer with 90 degree field ofregard, Proc. of SPIE Vol. 6971, 69710G, (2008)), SAW-based steering (asin CS Tsai et al., Guided-Wave Two Dimensional Acousto-Optic ScannerUsing Proton-Exchanged Lithium Niobate Waveguide, Fiber and IntegratedOptics 17, 157 (1998)), wavelength tuning accompanied by a pair ofdiffraction gratings, and so on. In other variations, a surface acousticwave beam may be displaced instead of the laser beam of input light 101,or the beam of input light 101 may be steered instead of (or in additionto) displacing it, and so on.

At the other end, a series of IDT's 110 generate the SAWs the propagatealong waveguides 102. RF controller 405 generates RF input signals 130-1. . . 130-N for each of the IDTs 110-1 . . . 110-N.

In specific embodiments, all of the waveguides 102 may be strobedsimultaneously or in a sequence. Additionally, the waveguides 102 can beincluded in different groupings. In this way, the waveguides 102 withineach group might be strobed simultaneously, and the different groupsstrobed sequentially, in another example.

Alternatively, if the strobe lights illuminate different waveguides insequence rather than simultaneously, a single large SAW transducer 110can produced the SAW's for multiple waveguides, or many SAW transducers110 may be coupled to a single RF input signal 130 feed.

FIG. 13B illustrates a different embodiment. The beam displacer or beamswitch 905 is replaced with a beam splitter 906. It divides the inputlight 101 from input light source 902 equally into the waveguides 102-1to 102-N. This allows one light source to drive multiple SAW devices200. In one embodiment, the splitter is formed by waveguide formed in oron the SAW substrate 120.

It also may be helpful to account for speed-of-sound frequencydispersion, for acoustic attenuation with distance, and for opticalattenuation with distance (due partly to SAW scattering) when encodingthe waveform of the RF light signals 130. This may be done with higheraccuracy by calibrating each unit separately, controlling the unit'stemperature and/or measuring the unit's temperature to adjust thecorrections.

In the specific application of a 3D display system 920, there may be twoadditional optical polarizers—one optical polarizer between the lightinput element and the SAW optical modulator 200, and the other opticalpolarizer at the exit face. It is noted that in this context, leaky modeSAW optical modulators have the property of placing the exit light 150in a polarization state that is rotated with respect to the relativelyhigh level of background noise that is present from non-modulated lightreflecting within the modulator.

U.S. Pat. No. 6,927,886, to Plesniak et al., incorporated herein byreference, hereinafter known as Plesniak, describes software tomanipulate the viewability of a holographic image. FIG. 14 is also FIG.11A in Plesniak.

In FIG. 14, relationships between a modulator plane 1110, a spatiallydistinct image plane 1120, and a viewzone 1130 are shown. The imagedepth 1140 and the hologram depth 1150 are also shown. Using embodimentsof the proposed system, optical power can be added by virtue of hardwareembodiments not just for the expansion (or contraction) of the output'sangular subtense, but to effectively “throw” the vertex of the outputfan towards or behind the modulator plane 1110 itself. This has benefitin fields such as holographic display, in which the perceived resolutiondrops with distance from the display. The image as viewed from the viewzone is formed in the image plane 1120. By adding or subtracting opticalpower, a surface of best resolution can be created at surfaces otherthan the modulator's exit face(s). Operation in this context isdescribed, for example, in Plesniak et al., “Reconfigurable imageprojection holograms,” Opt. Eng., vol. 45(11), (2006). In an arrangementof this sort, diffraction gratings, or the additional refractive orreflective optical element(s), can be “tuned” during manufacture orcomputationally to best match the features of the reconstructedholographic imagery, when the SAW device is used as a component of anelectronic display.

In accordance with embodiments of the present invention, an opticalengine of electro-holographic displays may be provided, such as: adesktop 3-D computer display, a head-worn near-eye virtualreality/augmented reality/mixed reality display, a virtual sand table,or the walls of a room creating immersive imagery. Applications of suchdisplays include: battlefield visualization, interventional medicalimaging for procedure planning and guidance, molecular visualization,and entertainment.

Electro-Holographic Display Architecture

FIG. 15 shows multiple electro-holographic light field generator devices300 stacked to form an electro-holographic 3D display 900, according toone embodiment.

In more detail, edge-fire SAW optical modulators 200 are employed in theelectro-holographic light field generator devices 300. In an edge-fireSAW device 200, the exit light 150 is emitted out the end face 170 ofeach optical modulator 200 of the stacked light field generator devices300. Further, these SAW optical modulators 200 preferably utilizenon-orthogonal end faces 170.

The light field generator devices 300 have longitudinal axes, defined bythe direction of the waveguide 102 of the SAW modulator devices 200 thatform the light field generator devices 300. These axes are parallel toline 914. Further, the light field generator devices 300 are arranged ina stack 901 such that the direction of their longitudinal axes 914 is atan angle 922 to the direction 912 of observers 910. Typically, the angle922 is between 20 and 70 degrees.

Moreover, the light field generator devices 300 are arranged, one on topof the other, such that the distal faces 168 of the modulator devices200 of one light field generator device 300 are adjacent to the proximalface 160 of the modulator devices 200 of the next light field generatordevice 300. Moreover, the end faces 170 of the separate SAW devices 200,generator devices 300 all lie in approximately the same verticallyextending plane.

FIG. 16A shows electro-holographic light field generator devices 300stacked to form an electro-holographic 3D display 900, according toanother embodiment.

This embodiment also employs edge-fire SAW optical modulators 200 in theelectro-holographic light field generator devices 300. And, theseoptical modulators 200 preferably utilize non-orthogonal end faces 170in which the edge cut angles are acute. In this example, however, thelongitudinal axis 914 of each of the modulator devices 200 is pointed atthe observers 910, such that angle 922 is less than 15 degrees, andpossibly 0 degrees.

Moreover, the light field generator devices 300 are arranged in a stack901, in pairs 340. Two pairs 340-1 and 340-2 within the stack 901 oflight field generator devices 300 are shown.

In each pair 340, the proximal faces 160 of the modulator devices200/light field generator devices 300 are adjacent to each other. Thepairs 340 are then stacked such that the distal faces 168 of themodulator devices 200 of one pair 340-1 are adjacent to the distal faces168 of the modulator devices 200 of the next pair 340-1 in the stack901.

FIG. 16B also shows electro-holographic light field generator devices300 stacked to form an electro-holographic 3D display 900, according toanother embodiment.

This embodiment also employs edge-fire SAW optical modulators 200 in theelectro-holographic light field generator devices 300. And, theseoptical modulators 200 preferably utilize non-orthogonal end faces 170,but here the edge cut angles are obtuse.

FIG. 17 shows a 3D display system 920. The 3D display system 920includes an electro-holographic 3D display 900 and also includesadditional components. The additional components include an illuminationsource 902, an RF driver 907, and a processor 909. Here, theelectro-holographic light field generator devices 300 of theelectro-holographic 3D display 900 are arranged in a dual column stack901. The light field generator devices 300 are stacked and arranged sideby side to obtain a 3D display system 920 with a wider display field inthe lateral direction.

Each of the electro-holographic light field generator devices 300 withinthe electro-holographic 3D display 900 receives a beam of input light101 generated by illumination source 902. The illumination source 902might be a laser such as a pulsed laser, to cite one of many possibleexamples of illumination light sources 902. The laser might illuminatethe generator devices 300 together in a beam. Separate in-couplingprisms could be used to couple light into each of the separatewaveguides.

The light field generator devices 300 are driven by the RF driver 907(also referred to herein as a “controller”). The RF driver 907 isgoverned by processor 909 on the basis of typically digitized graphicaldata resident or derived in a format appropriate for the electro-opticalsubsystem of the light field display 900. The 3D display system 920produces a modulated exit beam 930, in accordance with any of theteachings provided herein above, such that observers 910 in the farfield perceive an object 950 to be projected in three dimensions.

It is to be understood that the teachings presented herein may beapplied to SAW device 200 configurations described herein but may alsobe applied to any other SAW device 200 configurations, whether currentlyknown or developed in the future.

It is also important to note that such light field generators 900,though described in the specific context of 3D display systems, also canusefully be applied to other applications such as optogenetics, 3Dprinting, cloaking, and near-eye displays for augmented reality/virtualreality (AR/VR).

Embodiments of the invention may be implemented in part in anyconventional computer programming language such as VHDL, SystemC,Verilog, ASM, Python, C, C++, MATLAB etc. Alternative embodiments of theinvention may be implemented as pre-programmed hardware elements suchas, without limitation, combinations of one or more of afield-programmable gate array (FPGA), graphics processing unit (GPU),central processing unit (CPU) and other related components, or as acombination of hardware and software components.

Embodiments can be implemented in part as a computer program product foruse with a computer system. Such implementation may include a series ofcomputer instructions fixed either on a tangible medium, such as acomputer readable medium (e.g., a diskette, CD-ROM, ROM, or fixed disk)or transmittable to a computer system, via a modem or other interfacedevice, such as a communications adapter connected to a network over amedium. The medium may be either a tangible medium (e.g., optical oranalog communications lines) or a medium implemented with wirelesstechniques (e.g., microwave, infrared or other transmission techniques).The series of computer instructions embodies all or part of thefunctionality previously described herein with respect to the system.Those skilled in the art should appreciate that such computerinstructions can be written in a number of programming languages for usewith many computer architectures or operating systems. Furthermore, suchinstructions may be stored in any memory device, such as semiconductor,magnetic, optical or other memory devices, and may be transmitted usingany communications technology, such as optical, infrared, microwave, orother transmission technologies. It is expected that such a computerprogram product may be distributed as a removable medium withaccompanying printed or electronic documentation (e.g., shrink wrappedsoftware), preloaded with a computer system (e.g., on system ROM orfixed disk), or distributed from a server or electronic bulletin boardover the network (e.g., the Internet or World Wide Web). Of course, someembodiments of the invention may be implemented as a combination of bothsoftware (e.g., a computer program product) and hardware. Still otherembodiments of the invention are implemented as entirely hardware, orentirely software (e.g., a computer program product).

IDT Architecture

FIG. 18A shows detail for a prior art IDT 110.

In the ‘slab’ configuration which waveguide 102 assumes in FIG. 1A, theIDT 110 is comprised of transducer fingers 188. These transducer fingers188 are typically patterned at a higher layer than the waveguide 102,rather than at the same layer as the waveguide. As a result, sound waves(e.g. the surface acoustic waves 140) propagate at a lower “altitude”than the IDTs. Embodiments of the SAW devices 200 disclosed herein mightutilize an IDT 110 having transducer fingers 188 in accordance with FIG.18A.

FIG. 18B through FIG. 18G show different layouts of transducer fingers188 that can be constructed for the various embodiments of the SAWdevices 200 proposed herein.

FIG. 18B, for example, shows transducer fingers 188 of a waveguide thatuses the geometry of a channel rather than that of the ‘slab’configuration of the waveguide shown in FIG. 1A. The transducer fingers188 are disposed astride the channel waveguide 102. Longitudinalacoustic wave 189 is shown propagating in the channel waveguide 102. Thechannel waveguide 102 may support multiple modes of electromagneticradiation. Here, the configuration of the transducer fingers 188 mayadvantageously provide enhanced electro-mechanical efficiency whencompared with the prior art slab configuration of FIG. 18A.

FIG. 18C shows a view similar to that of FIG. 18B, additionallydepicting an emergent fan of deflected exit light 150. FIG. 18D shows aside view of the transducer fingers 188 in FIGS. 18B and 18C, and alsoshows diffracted light 162 inside substrate 120 which emerge as rays ofexit light 150 outside the substrate 120.

In the embodiment shown in FIG. 18F, multiple waveguides 102 may bepatterned into the material used for SAW device 200, such as lithiumniobate, for example. Light used to illuminate multiple waveguides 102as shown in FIG. 18F may also be derived from a single input lightsource 902. FIG. 18G is a cross-sectional side view of either of theembodiments of FIG. 18E or 18F.

While this invention has been particularly shown and described withreferences to preferred embodiments thereof, it will be understood bythose skilled in the art that various changes in form and details may bemade therein without departing from the scope of the inventionencompassed by the appended claims.

What is claimed is:
 1. An electro-holographic light field generatordevice, comprising: a substrate; an array of surface acoustic wavemodulators having waveguides extending across the substrate; and twodimensional array of diffractive optics for shaping output light fromthe substrate.
 2. The device as claimed in claim 1, wherein thewaveguides extend parallel to each other across the substrate.
 3. Thedevice as claimed in claim 1, wherein a separation between thewaveguides is less than 400 μm.
 4. The device as claimed in claim 1,wherein a length of the waveguides is less than 10 centimeters.
 5. Thedevice as claimed in claim 1, wherein different ones of the waveguidescarry different colors of light.
 6. The device as claimed in claim 1,wherein the array of optics is on a face of the substrate.
 7. The deviceas claimed in claim 1, wherein the array of optics is on an exit face ofthe substrate.
 8. The device as claimed in claim 1, wherein the array ofoptics is an array of diffractive lenses.
 9. The device as claimed inclaim 8, wherein the diffractive lenses are arranged into lens strips,one strip for each waveguide.
 10. The device as claimed in claim 1,wherein a length of each of the diffractive lenses is less than 2millimeters.
 11. The device as claimed in claim 1, wherein the array ofoptics is an array of chirped gratings.
 12. A modulator as claimed inclaim 1, wherein the optic is formed on a distal face of the substrate.13. A modulator as claimed in claim 1, wherein the optic increases anexit angle fan of the light from the substrate.
 14. A modulator asclaimed in claim 1, wherein the array of surface acoustic wavemodulators includes multiple SAW transducers.
 15. A modulator as claimedin claim 1, wherein each of the optics of the array has a length of 100μm-2 mm.
 16. A modulator as claimed in claim 1, wherein the substrateincludes at least three surface acoustic wave modulators.
 17. Amodulator as claimed in claim 1, wherein the substrate includes twelvesurface acoustic wave modulators.